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Multi Pulse Propulsion
General
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Dual-pulse motors are very promising candidates
for the next generation of missiles. The key characteristic of the motor
is the management of different thrust impulses according to mission need.
The pulse management is performed by several propellant charges separated
by a frangible bulkhead or a soft membrane, where the charges can be ignited
separately. The feasibility of throttleable rocket motors using a variable
throat is studied.
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